作者: G. Clark
DOI: 10.1016/0010-4361(89)90335-2
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摘要: Abstract A previous investigation into the characteristics of impact damage in carbon fibre laminates indicated that delaminations occur preferentially at certain interfaces. model is proposed which explains distribution these preferred interfaces, as well some damage, such relative size and occurrence prominent delamination/cracking features. study delamination growth under fatigue loading indicates a tendency for directions to be defined by initial (and predictable) structure damaged zone.